Air Power Series>1:72 die-cast display model>F-18>HA3531
McDonnell Douglas F/A-18B A21-103, 3 Squadron., RAAF, 2006
General Background
The McDonnell Douglas (now Boeing) F/A-18 Hornet is a supersonic twin engine all-weather night fighter and attack aircraft. The F/A-18s first flew in November 1978 and the first production flight on April 12, 1980. The first 380 aircraft were F/A-18As and in September 1987 production switched to the F/A-18C. Variants A and C are single-seat aircraft while B and D are tandem-seats. The Hornet can operate from either aircraft carriers or land bases with the capability of in flight refueling. A total of 1,480 A-D variants were built.
The Aircraft
RAAF F/A-18B serial A21-103 was built as c/n 0215/ATF103 and along with A21-104 were flown by C-5 Galaxy to Australia arriving on June 6, 1984. These two aircraft were re-assembled and when A21-103 rolled out on November 16, 1984 it was considered the first Australian built Hornet. After flight testing A21-103 was delivered to 20 CU (Conversion Unit) at Williamtown on May 17, 1985. On January 1, 2005 the aircraft was with the RAAF 3 Squadron at Williamtown.
Specifications :
| Role: | Fighter/Attack |
| Manufactured: | 1980 to 1987 |
| Numbers Produced: | A – 371 |
| B – 40 | |
| Crew: | A – 1 |
| B – 2 | |
| Dimensions | |
| Length: | 56 ft 0 in (17.07 m) |
| Wingspan: | 40 ft 8 in (12.4 m) |
| Folded: | 27 ft 6 in (8.38 m) |
| Height: | 15 ft 4 in (4.66 m) |
| Weight: | |
| Empty: | 28,000 lbs (12,700 kg) |
| Gross: | 38,000 lbs (17,240 kg) |
| Maximum Take off: | 56,000 lb (25,400 kg) |
| Performance | |
| Engines: | 2 X GE F404-GE turbofans producing 10,600 lb.s.t. dry & 15,800 lb.s.t with afterburning per engine |
| Fuel: | |
| Internal: | 1,670 U.S. gal (6,322 l) |
| External: | As many as 3 X 330 U.S. gal (1,249 l) drop tanks |
| Maximum Fuel: | 2,660 U.S. gal (10,070 l) |
| Maximum Speed: | Mach 1.8 1,190 mph (1,915 km/h) @ 35,000 ft (10,670 m) |
| Landing Speed: | 150 mph (241.4 km/h) |
| Combat Ceiling: | 50,000 ft (15,240 m) |
| Maximum Range: | 2,875 miles (4,627 km) |
| Armament: | 1 X 20 mm M61A1 cannon in nose Plus |
| Hard Points: | 4 X under-wing |
| 2 X fuselage corner stations | |
| 1 X center-line | |
| 2 X wing-tip | |
| To carry AIM-9 Sidewinder Missiles Or | |
| AIM-7 Sparrow Missiles Plus | |
| Up to 3 external fuel tanks and other assorted ordnance |